JP2018530720A - Reducer load distribution with two intermediate transmission lines - Google Patents

Reducer load distribution with two intermediate transmission lines Download PDF

Info

Publication number
JP2018530720A
JP2018530720A JP2018516059A JP2018516059A JP2018530720A JP 2018530720 A JP2018530720 A JP 2018530720A JP 2018516059 A JP2018516059 A JP 2018516059A JP 2018516059 A JP2018516059 A JP 2018516059A JP 2018530720 A JP2018530720 A JP 2018530720A
Authority
JP
Japan
Prior art keywords
input line
line
speed reducer
gear
damping means
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2018516059A
Other languages
Japanese (ja)
Other versions
JP6839704B2 (en
Inventor
マチュー，アントワーヌ
フェロー，バンジャマン
モレリ，ボリス
アミエット，マクシム
Original Assignee
サフラン・トランスミッション・システムズ
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by サフラン・トランスミッション・システムズ filed Critical サフラン・トランスミッション・システムズ
Publication of JP2018530720A publication Critical patent/JP2018530720A/en
Application granted granted Critical
Publication of JP6839704B2 publication Critical patent/JP6839704B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H35/00—Gearings or mechanisms with other special functional features
    • F16H35/06—Gearings designed to allow relative movement between supports thereof without ill effects
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H4/00—Swimming or splash baths or pools
    • E04H4/0018—Easily movable or transportable swimming pools
    • E04H4/0031—Easily movable or transportable swimming pools with shell type elements
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H4/00—Swimming or splash baths or pools
    • E04H4/0018—Easily movable or transportable swimming pools
    • E04H4/0043—Easily movable or transportable swimming pools mainly made of panels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/12—Combinations with mechanical gearing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/16—Suppression of vibrations in rotating systems by making use of members moving with the system using a fluid or pasty material
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H1/00—Toothed gearings for conveying rotary motion
    • F16H1/02—Toothed gearings for conveying rotary motion without gears having orbital motion
    • F16H1/20—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H1/00—Toothed gearings for conveying rotary motion
    • F16H1/02—Toothed gearings for conveying rotary motion without gears having orbital motion
    • F16H1/20—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members
    • F16H1/22—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/02—Gearboxes; Mounting gearing therein
    • F16H57/021—Shaft support structures, e.g. partition walls, bearing eyes, casing walls or covers with bearings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112—Single lapped joints
    • B29C66/1122—Single lap to lap joints, i.e. overlap joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/114—Single butt joints
    • B29C66/1142—Single butt to butt joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/10—Building elements, e.g. bricks, blocks, tiles, panels, posts, beams
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/52—Sports equipment ; Games; Articles for amusement; Toys
    • B29L2031/5254—Swimming or diving equipment
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H4/00—Swimming or splash baths or pools
    • E04H4/0018—Easily movable or transportable swimming pools
    • E04H2004/0068—Easily movable or transportable swimming pools made of plastic shells or plastic elements including at least parts of walls and floors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/312—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being parallel to each other
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/0004—Joining sheets, plates or panels in abutting relationship
    • F16B5/0056—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates or panels or the interlocking key perpendicular to the main plane
    • F16B5/0068—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates or panels or the interlocking key perpendicular to the main plane and using I-shaped clamps with flanges moving towards each other
    • F16B5/0072—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates or panels or the interlocking key perpendicular to the main plane and using I-shaped clamps with flanges moving towards each other and using screw-thread
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Abstract

本発明は、入力ライン（１２）と、中間ラインを介して入力ラインによって駆動される出力ライン（１４）とを含む、特にタービンエンジン用の２つの中間伝達ライン（１６）を持つ減速機（１０）にして、前記中間ラインが実質的に平行である減速機（１０）であって、前記中間ラインの間に負荷分配手段を含み、前記負荷分配手段が、入力ラインの第１の端部を回転自在に結合するためのボールソケット手段（３０）と、入力ラインの前記端部の半径方向の動きを減衰させるための第１の手段（３４）と、入力ラインの第２の反対側の端部の半径方向の動きを減衰させるための第２の手段（３４）と、を備えることを特徴とする減速機（１０）に関する。  The invention comprises a reduction gear (10) having two intermediate transmission lines (16), in particular for a turbine engine, comprising an input line (12) and an output line (14) driven by the input line via the intermediate line. ), Wherein the intermediate line is substantially parallel, and includes a load distribution means between the intermediate lines, the load distribution means connecting the first end of the input line. Ball socket means (30) for rotationally coupling; first means (34) for dampening radial movement of said end of the input line; and second opposite end of the input line And a second means (34) for attenuating the radial movement of the part, relating to a speed reducer (10).

Description

本発明は、特にターボ機械のための、２つの中間伝達ラインを持つ減速機に関する。   The present invention relates to a speed reducer with two intermediate transmission lines, especially for turbomachines.

従来技術は、特に、文献米国特許第３７７２９３４号明細書、欧州特許出願公開第０６３６８１３号明細書、および国際公開第２０１３／１５０２２９号を含む。   The prior art includes, inter alia, the documents US Pat. No. 3,772,934, European Patent Application Publication No. 0636813, and International Publication No. 2013/150229.

ターボ機械は、１つまたは複数の機械的減速機を備えることができる。これは、特に、プロペラが減速機を使ってタービンシャフトによって回転させられるターボプロップエンジン機の場合である。   A turbomachine may comprise one or more mechanical reducers. This is especially the case for turboprop engine machines where the propeller is rotated by a turbine shaft using a speed reducer.

遊星歯車減速機構、チェーン歯車、ウォームギア、中間伝達ライン、等のような、多くの種類の減速機がある。本発明は、主として、伝達ラインを持つ減速機（複合減速機とも呼ばれる）に関する。   There are many types of reducers, such as planetary gear reduction mechanisms, chain gears, worm gears, intermediate transmission lines, and so on. The present invention mainly relates to a reduction gear having a transmission line (also called a compound reduction gear).

現在の技術においては、この種の減速機は、入力ラインと２つの中間伝達ラインを使って入力ラインによって駆動される出力ラインとを備える。入口ラインによって伝達される動力は、出力ラインに伝達される前に中間ラインの間で分割される。中間伝達ラインは、平行であり、一般に、入力ラインと噛み合う入力歯車および出力ラインと噛み合う出力歯車を担持するシャフトをそれぞれ備える。異なる歯車の歯数を変化させることによって、入力ラインと出力ラインとの間の減速比を得ることができる。この構造は、限られた空間において、および制御された質量によって大きな減速が可能である。   In current technology, this type of reducer comprises an input line and an output line driven by the input line using two intermediate transmission lines. The power transmitted by the inlet line is split between the intermediate lines before being transmitted to the output line. The intermediate transmission lines are parallel and generally each include a shaft carrying an input gear meshing with the input line and an output gear meshing with the output line. By changing the number of teeth of different gears, the reduction ratio between the input line and the output line can be obtained. This structure can be greatly decelerated in a limited space and with a controlled mass.

定義により、この種の減速機は、不静定システムである。特定の構成がなければ、一方の中間ラインはモータ動力の大部分にこれを通過させることができるが、他方の中間ラインは事実上いかなる動力の流れも起こらない。   By definition, this type of reducer is an indeterminate system. Without a specific configuration, one intermediate line can pass most of the motor power through, while the other intermediate line does not cause virtually any power flow.

したがって、動力の半分が減速機の中間ラインの各々を通過することを確実にするように、上述の種類の減速機の中間ラインの間に負荷を分配させる必要性が存在する。   Therefore, there is a need to distribute the load between the intermediate lines of the above-described types of reducers to ensure that half of the power passes through each of the intermediate lines of the reducer.

１つの解決策は、入力ラインの１つの端部を旋回結合するためのボールソケット手段と、入力ラインの反対側の端部の半径方向の動きを減衰させるための手段とを設けることから成る。   One solution consists of providing ball socket means for pivoting one end of the input line and means for dampening radial movement of the opposite end of the input line.

入力ラインは、（その長手方向軸線に対して）半径方向に動きやすい。これは、たとえば、モータシャフトに関して、入力ラインの端部の１つが旋回可能に取り付けられることによって可能になる。したがって、入力ラインの反対側の端部は、半径方向に動くことができ、これらの動きは減衰される。旋回および減衰のためのこれらの手段は、負荷を分配させるための手段を形成し、これは、次のように機能する。中間ラインの一方がより多く負荷される、すなわち、このラインを通過するトルクが他方のラインを通過するトルクより大きいならば、この場合、トルクによって生成される入力ラインの歯車の応力は、一方の側が他方よりも大きい。したがって、力が入力歯車に加えられることになり、これは、入力ラインの半径方向の動きをもたらすことになる。この動きにより、遊びが入力ラインのレベルで再平衡されるようになっている。平衡されると、中間ラインのトルクによって歯車に置かれる応力は相殺し、これは、中間ラインのトルクが等しいことを意味する。   The input line is easy to move in the radial direction (relative to its longitudinal axis). This is possible, for example, with respect to the motor shaft by one of the ends of the input line being pivotally mounted. Thus, the opposite end of the input line can move radially and these movements are attenuated. These means for swiveling and damping form a means for distributing the load, which functions as follows. If one of the intermediate lines is more heavily loaded, i.e. the torque passing through this line is greater than the torque passing through the other line, then the input line gear stress produced by the torque will be The side is larger than the other. Thus, a force will be applied to the input gear, which will result in radial movement of the input line. This movement causes play to be rebalanced at the input line level. When balanced, the stress placed on the gear by the midline torque cancels out, which means that the midline torque is equal.

しかしながら、この解決策は、歯車のミスアライメントを招く場合がある。この整列してない動作が原因で、ギア歯の「クラウニング」型の補正が必要とされる。この補正は、歯の面圧の増加を招く。加えて、ミスアライメントが大きな影響を与える場合は、たとえクラウニングを適用しても、必ずしも減速機の許容可能な動作を確実にすることができるとは限らない。   However, this solution may lead to gear misalignment. Due to this misaligned movement, a "crowning" type correction of the gear teeth is required. This correction leads to an increase in tooth surface pressure. In addition, if misalignment has a significant impact, even if crowning is applied, it is not always possible to ensure acceptable operation of the reducer.

米国特許第３７７２９３４号明細書U.S. Pat. No. 3,772,934 欧州特許出願公開第０６３６８１３号明細書European Patent Application No. 0636813 国際公開第２０１３／１５０２２９号International Publication No. 2013/150229

本発明は、上述の問題に対する簡単で効率的で経済的な解決策を提案する。   The present invention proposes a simple, efficient and economical solution to the above problem.

本発明は、入力ラインと、中間ラインを使って入力ラインによって駆動される出力ラインとを備える、特にターボ機械用の２つの中間伝達ラインを持つ減速機にして、これらの中間ラインが実質的に平行である減速機であって、前記中間ラインの間に負荷を分配する手段を備え、この負荷分配の手段が、入力ラインの第１の端部を旋回結合するためのボールソケット手段と、入力ラインの前記第１の端部の半径方向の動きを減衰させるための第１の手段と、入力ラインの第２の反対側の端部の半径方向の動きを減衰させるための第２の手段と、を備えることを特徴とする、減速機に関する。   The present invention provides a reducer having two intermediate transmission lines, in particular for turbomachines, comprising an input line and an output line driven by the input line using the intermediate line. A reduction gear that is parallel and comprises means for distributing a load between said intermediate lines, said means for distributing load being ball socket means for pivotally coupling the first end of the input line; First means for attenuating radial movement of the first end of the line; and second means for attenuating radial movement of the second opposite end of the input line; The present invention relates to a speed reducer.

本発明の背後にある原理は、入力ラインを２つの離れている減衰手段に取り付けることである。本発明により、入力ラインがミスアライメントなしに垂直に動くことができるようになっている。   The principle behind the present invention is to attach the input line to two separate damping means. The present invention allows the input line to move vertically without misalignment.

本発明による減速機は、分離してまたは互いに組み合わさって適用される次の特徴のうちの１つまたはいくつかを含むことができ：
前記第１および第２の減衰手段は、入力ラインが中間ラインの軸線を実質的に通過する平面にほぼ垂直な方向に動くことができるように構成され、
前記第１および第２の減衰手段は、ばね、好ましくは戻しばねを備え、
前記ばねは、同一であり、
前記第１および第２の減衰手段は、ころ軸受を備え、
前記第１および第２の減衰手段の各々は、入力ラインの前記第１または第２の端部に取り付けられるころ軸受を備え、このころ軸受が、ばねによって支持され、
前記第１および第２の減衰手段は、同一であり、
前記第１および第２の減衰手段は、入力ラインの歯車の両側に取り付けられ、
前記第１および第２の減衰手段（）は、前記歯車から等距離に位置しており、ローラは、各ローラ上で同じ動きをするように、したがって歯のミスアライメントを回避するようにギア歯から等距離に配置され得る。 The speed reducer according to the present invention can include one or several of the following features applied separately or in combination with each other:
The first and second attenuation means are configured such that the input line can move in a direction substantially perpendicular to a plane substantially passing through the axis of the intermediate line;
The first and second damping means comprise springs, preferably return springs,
The springs are identical;
The first and second damping means comprise roller bearings;
Each of the first and second damping means comprises a roller bearing attached to the first or second end of the input line, the roller bearing being supported by a spring,
The first and second damping means are identical;
The first and second damping means are mounted on opposite sides of the input line gear;
The first and second damping means () are located equidistant from the gear and the gear teeth so that the rollers have the same movement on each roller and thus avoid tooth misalignment. Can be placed equidistant from each other.

また、本発明は、上述のような少なくとも１つの減速機を備えることを特徴とする、ターボ機械に関する。減速機は、ターボ機械によって流線型にされていないプロペラを駆動するように構成される出力ラインを備えることができる。   The present invention also relates to a turbomachine comprising at least one speed reducer as described above. The reducer can include an output line configured to drive a propeller that has not been streamlined by the turbomachine.

好ましくは、ターボ機械は航空機ターボプロップエンジン機である。   Preferably, the turbomachine is an aircraft turboprop engine.

本発明は、非限定的な実施例として、また添付の図面を参照して次の説明を読むとよりよく理解されるであろうし、本発明の他の詳細、特徴、および利点が明らかになるであろう。   The invention will be better understood as a non-limiting example and by reading the following description with reference to the accompanying drawings, and other details, features and advantages of the invention will become apparent. Will.

側面から見た、２つの中間伝達ラインを持つ減速機の非常に概略的な図である。FIG. 3 is a very schematic view of a reduction gear with two intermediate transmission lines as seen from the side. 正面から見た、２つの中間伝達ラインを持つ減速機の非常に概略的な図である。FIG. 3 is a very schematic view of a reduction gear with two intermediate transmission lines as seen from the front. 中間ラインの間の負荷の不均一な配分を示す、説明した種類の減速機の正面から見た部分概略図である。FIG. 3 is a partial schematic view from the front of a reducer of the kind described, showing the uneven distribution of the load between the intermediate lines. 中間ラインの間の負荷の均一な配分を示す、説明した種類の減速機の正面から見た部分概略図である。FIG. 3 is a partial schematic view from the front of a reduction gear of the kind described, showing a uniform distribution of the load between the intermediate lines. 負荷分配手段を備えた入力ラインの非常に概略的な図である。FIG. 2 is a very schematic diagram of an input line with load distribution means. 本発明による負荷分配手段を備えた入力ラインの非常に概略的な図である。FIG. 3 is a very schematic diagram of an input line with load distribution means according to the invention.

図１は、２つの中間伝達ラインを持つ減速機１０を非常に概略的に示しており、前記減速機１は、主として、４つの部分、すなわち入力ライン１２と、出力ライン１４と、入力ライン１２によって駆動され、次には出力ライン１４を駆動する２つの中間伝達ライン１６とを備える。   FIG. 1 very schematically shows a speed reducer 10 with two intermediate transmission lines, said speed reducer 1 mainly comprising four parts: an input line 12, an output line 14, and an input line 12. And then two intermediate transmission lines 16 for driving the output line 14.

減速機の異なる部分１２、１４、１６は、一般に、ここには示されていない減速機ケーシングに取り付けられ、この減速機は、たとえば入力ラインの通過、およびターボ機械の第１の構成要素へのその接続のための第１の開口部と、出力ラインの通過、およびターボ機械の第２の構成要素へのその接続のための第２の開口部とを備える。たとえば、第１の構成要素は、ターボ機械のタービンシャフトであり、第２の構成要素は、ターボ機械がターボプロップエンジン機である場合にはそのターボ機械のプロペラの駆動シャフトである。   The different parts 12, 14, 16 of the speed reducer are generally attached to a speed reducer casing, not shown here, which is for example passed through the input line and to the first component of the turbomachine. A first opening for the connection and a second opening for the connection of the output line and the connection to the second component of the turbomachine. For example, the first component is the turbine shaft of a turbomachine and the second component is the drive shaft of the turbomachine propeller if the turbomachine is a turboprop engine.

入力ライン１２は、外歯を持つ歯車２０を担持するシャフト１８を含む。歯車２０およびシャフト１８は、同軸であり、Ｂとマークされた同じ軸線を中心として回転する。   The input line 12 includes a shaft 18 that carries a gear 20 having external teeth. Gear 20 and shaft 18 are coaxial and rotate about the same axis marked B.

出力ライン１４は、外歯を持つ歯車２４を担持するシャフト２２を含む。歯車２４およびシャフト２２は、同軸であり、Ａとマークされた同じ軸線を中心として回転する。この場合に、これらは、歯車２０および入力ラインのシャフト１８と同じ回転方向に回転する。   The output line 14 includes a shaft 22 that carries a gear 24 having external teeth. Gear 24 and shaft 22 are coaxial and rotate about the same axis marked A. In this case, they rotate in the same rotational direction as the gear 20 and the shaft 18 of the input line.

入力ライン１２および出力ライン１４は、平行である。したがって、それらの回転軸線Ａ、Ｂは、平行である。   The input line 12 and the output line 14 are parallel. Therefore, their rotation axes A and B are parallel.

中間伝達ライン１６は、実質的に平行であり、同一である。各ライン１６は、第１の端部で入力歯車２６を、および第２の端部で出力歯車２８を担持するシャフト２５を備える。出力歯車２８は、出力ライン１４の歯車２４と噛み合う。入力歯車２６は、入力ライン１２の歯車２０と噛み合う。歯車２６、２８は、外歯を有する。各シャフト２５およびその歯車２６、２８は、同軸であり、軸線ＡおよびＢに平行な、Ｃとマークされた同じ軸線を中心として回転する。   The intermediate transmission lines 16 are substantially parallel and identical. Each line 16 includes a shaft 25 that carries an input gear 26 at a first end and an output gear 28 at a second end. The output gear 28 meshes with the gear 24 of the output line 14. The input gear 26 meshes with the gear 20 of the input line 12. The gears 26 and 28 have external teeth. Each shaft 25 and its gears 26, 28 are coaxial and rotate about the same axis marked C, parallel to axes A and B.

先に説明されたように、この種の減速機１０は、不静定システムであり、一方の中間ライン１６はモータ動力の大部分にこれを通過させることができるが、他方の中間ラインは、事実上いかなる動力の流れも起こらない。図２でお分かりのように、動力または負荷のこの不十分な分配は、主として、歯車２６は点Ｃで歯車２０と接触しており、また中間ラインの一方の歯車２８は点Ｄで歯車２４接触しているが、歯車２４と他方の中間ラインの歯車２８との間のＥで遊びがないことを確実にすることが困難であるという事実によるものである。   As explained earlier, this type of reducer 10 is an indeterminate system, with one intermediate line 16 allowing it to pass most of the motor power while the other intermediate line is Virtually no power flow occurs. As can be seen in FIG. 2, this inadequate distribution of power or load is primarily due to the fact that gear 26 is in contact with gear 20 at point C and one gear 28 in the intermediate line is gear 24 at point D. This is due to the fact that it is difficult to ensure that there is no play at E between the gear 24 and the gear 28 of the other intermediate line.

本発明は、減速機１０に中間ライン１６の間で負荷を分配するための手段を装備することによってこの問題に対する解決策を提案する。   The present invention proposes a solution to this problem by equipping the speed reducer 10 with means for distributing the load between the intermediate lines 16.

負荷の分配の一般的原理は、図３から図５に示されており、図６は、本発明の一実施形態を示している。   The general principle of load distribution is illustrated in FIGS. 3-5, and FIG. 6 illustrates one embodiment of the present invention.

入力ライン１２のシャフト１８は（その長手方向軸線に対して）半径方向に動きやすい。これは、たとえばタービンシャフトに関して、その端部の１つが旋回可能に取り付けられる（図５）ことによって可能になる。シャフト１８の端部は、たとえば、減速機の入力ラインをタービンシャフトに接続するスリーブ３２の相補的な溝に係合する旋回溝３０を備える。半径方向の動きは、この時に、その旋回端部のレベルに位置している点の周りの入力ライン１２の旋回として理解されるべきである。   The shaft 18 of the input line 12 is easy to move radially (relative to its longitudinal axis). This is possible, for example, with respect to the turbine shaft by one of its ends being pivotally mounted (FIG. 5). The end of the shaft 18 comprises, for example, a swivel groove 30 that engages a complementary groove in a sleeve 32 that connects the input line of the reducer to the turbine shaft. Radial movement is to be understood at this time as a swiveling of the input line 12 around a point located at the level of its swivel end.

したがって、入力ライン１２のシャフト１８の反対側の端部は、半径方向に動くことができ、これらの動きは、ばね３４によって減衰される。   Thus, the opposite end of the shaft 18 of the input line 12 can move radially and these movements are damped by the spring 34.

中間ライン１６の一方がより多く負荷される（図３）、すなわち、このラインを通過するトルクが他方のラインを通過するトルクより大きいならば、この場合、このトルクによって生成される入力ラインの歯車２０の応力ｆ１は、一方の側が他方よりも大きい。したがって、力Ｆが入力ラインの歯車２０に加えられることになり、これは、入力ラインの動きをもたらすことになる。この動きにより、遊びが入力ラインのレベルで再平衡されるようになっている。平衡されると、中間ラインのトルクによって歯車２０に置かれる応力ｆ１、ｆ２は相殺し、これは、中間ラインのトルクが等しいことを意味する。   If one of the intermediate lines 16 is loaded more (FIG. 3), ie the torque passing through this line is greater than the torque passing through the other line, in this case the input line gear produced by this torque The stress f1 of 20 is greater on one side than on the other. Thus, a force F will be applied to the input line gear 20, which will result in movement of the input line. This movement causes play to be rebalanced at the input line level. Once balanced, the stresses f1, f2 placed on the gear 20 by the intermediate line torque cancel, which means that the intermediate line torque is equal.

有利なことに、ばね３４の減衰手段は、入力ライン１２のシャフト１８を案内するころ軸受３６と組み合わされる。   Advantageously, the damping means of the spring 34 is combined with a roller bearing 36 that guides the shaft 18 of the input line 12.

上述のように、歯車のミスアライメントが、図５に示されるように発生する場合がある。この整列してない動作が原因で、ギア歯の「クラウニング」型の縦方向の補正が必要とされる。この補正は、歯の面圧の増加を招く。加えて、ミスアライメントが大きな影響を与える場合は、たとえクラウニングを適用しても、必ずしも減速機の許容可能な動作を確実にすることができるとは限らない。   As described above, gear misalignment may occur as shown in FIG. Due to this misaligned movement, a gear crown “crowning” type longitudinal correction is required. This correction leads to an increase in tooth surface pressure. In addition, if misalignment has a significant impact, even if crowning is applied, it is not always possible to ensure acceptable operation of the reducer.

本発明により、この問題が全体的な入力ライン減衰によって改善されるようになっている。   The present invention improves this problem by overall input line attenuation.

図６は、本発明の一実施形態の一実施例を示しており、その場合、上述の要素は同じ参照数字で示されている。   FIG. 6 shows an example of an embodiment of the present invention, in which the elements described above are indicated with the same reference numerals.

たとえばボール型の２つのころ軸受３６が、入力ライン１２の端部において歯車２０の両側に取り付けられる。   For example, two ball-shaped roller bearings 36 are attached to both sides of the gear 20 at the end of the input line 12.

古典的には、各軸受３６は、それぞれ内側および外側の２つのリングを備えることができ、その間にリング状の保持器によって保持され得る玉軸受の列が延在する。旋回溝３０を備えるその端部と反対側に、第１の軸受３６の内輪が入力ライン１２のシャフト１８の端部に固定して取り付けられる。第２の軸受３６の内輪は、旋回溝３０を備えるシャフト１８の端部に固定して取り付けられる。   Classically, each bearing 36 can comprise two inner and outer rings, respectively, between which extend a row of ball bearings that can be held by a ring-shaped retainer. The inner ring of the first bearing 36 is fixedly attached to the end of the shaft 18 of the input line 12 on the side opposite to the end provided with the turning groove 30. The inner ring of the second bearing 36 is fixedly attached to the end of the shaft 18 having the turning groove 30.

減衰ばね３４は、軸受３６を支持する。第１のばね３４は、第１の軸受３６を支持し、第２のばね３４は、第２の軸受３６を支持する。好ましくは、ばね３４は、同一である。好ましくは、ばねは、戻しばねである。有利なことに、それらは、歯車２０から等距離に位置している。   The damping spring 34 supports the bearing 36. The first spring 34 supports the first bearing 36, and the second spring 34 supports the second bearing 36. Preferably, the springs 34 are the same. Preferably, the spring is a return spring. Advantageously, they are located equidistant from the gear 20.

旋回溝３０を備えるシャフト１８の端部は、減速機の入力ラインをタービンシャフトに接続するスリーブ３２の相補的な溝に係合される。   The end of the shaft 18 with the swivel groove 30 is engaged in a complementary groove in the sleeve 32 that connects the reducer input line to the turbine shaft.

本発明は、図３および図４に関して先に述べたように機能する。図６に見られるように、中間ライン１６の一方がより多く負荷される（図３）、すなわち、そのラインを通過するトルクが他方のラインを通過するトルクより大きいならば、この場合、このトルクによって生成される入力ラインの歯車２０の応力ｆ１は、他方の側よりも大きい。したがって、力Ｆが入力ラインの歯車２０に加えられることになり、これは入力ラインの動きをもたらすことになるが、本発明のおかげで、これは位置ずれが生じることになることを意味しない。   The present invention functions as described above with respect to FIGS. As seen in FIG. 6, if one of the intermediate lines 16 is more heavily loaded (FIG. 3), ie if the torque passing through that line is greater than the torque passing through the other line, then this torque The stress f1 of the gear 20 of the input line generated by is greater than the other side. Thus, a force F will be applied to the input line gear 20, which will result in movement of the input line, but thanks to the present invention, this does not mean that a displacement will occur.

Claims (10)

入力ライン（１２）と、中間ラインを使って入力ラインによって駆動される出力ライン（１４）とを備える、特にターボ機械用の２つの中間伝達ライン（１６）を持つ減速機（１０）にして、これらの中間ラインが実質的に平行である減速機（１０）であって、前記中間ラインの間に負荷の分配の手段を備え、この負荷分配の手段が、入力ラインの第１の端部を旋回結合するためのボールソケット手段（３０）と、入力ラインの前記第１の端部の半径方向の動きを減衰させるための第１の手段（３４）と、入力ラインの第２の反対側の端部の半径方向の動きを減衰させるための第２の手段（３４）と、を備えることを特徴とする、減速機（１０）。   A reduction gear (10) with two intermediate transmission lines (16), in particular for turbomachines, comprising an input line (12) and an output line (14) driven by the input line using the intermediate line, A reduction gear (10), wherein these intermediate lines are substantially parallel, comprising means for load distribution between said intermediate lines, the load distribution means connecting the first end of the input line. Ball socket means (30) for pivotal coupling, first means (34) for dampening radial movement of the first end of the input line, and second opposite side of the input line A speed reducer (10), characterized by comprising second means (34) for dampening radial movement of the ends. 前記第１および第２の減衰手段（３４）が、入力ライン（１２）が中間ラインの軸線（Ｃ）を実質的に通過する平面にほぼ垂直な方向に動くことができるように構成される、請求項１に記載の減速機（１０）。   The first and second damping means (34) are configured such that the input line (12) can move in a direction substantially perpendicular to a plane substantially passing through the axis (C) of the intermediate line; The speed reducer (10) according to claim 1. 前記第１および第２の減衰手段（３４）が、ばね、好ましくは戻しばねを備える、請求項１または２に記載の減速機（１０）。   3. The speed reducer (10) according to claim 1 or 2, wherein the first and second damping means (34) comprise springs, preferably return springs. 前記ばねが、同一である、請求項３に記載の減速機（１０）。   The speed reducer (10) according to claim 3, wherein the springs are identical. 前記第１および第２の減衰手段（３４）が、ころ軸受を備える、請求項１から４のいずれか一項に記載の減速機（１０）。   The speed reducer (10) according to any one of claims 1 to 4, wherein the first and second damping means (34) comprise roller bearings. 前記第１および第２の減衰手段（３４）の各々が、入力ラインの前記第１または第２の端部に取り付けられるころ軸受を備え、このころ軸受が、ばねによって支持される、請求項４に従属する請求項５に記載の減速機（１０）。   Each of said first and second damping means (34) comprises a roller bearing attached to said first or second end of an input line, said roller bearing being supported by a spring. The speed reducer (10) according to claim 5, which is dependent on. 前記第１および第２の減衰手段（３４）が、同一である、請求項１から６のいずれか一項に記載の減速機（１０）。   The speed reducer (10) according to any one of claims 1 to 6, wherein the first and second damping means (34) are identical. 前記第１および第２の減衰手段（３４）が、入力ライン（１２）の歯車（２０）の両側に取り付けられる、請求項１から７のいずれか一項に記載の減速機（１０）。   The speed reducer (10) according to any one of the preceding claims, wherein the first and second damping means (34) are mounted on both sides of the gear (20) of the input line (12). 前記第１および第２の減衰手段（３４）が、前記歯車から等距離に位置している、請求項８に記載の減速機（１０）。   The speed reducer (10) according to claim 8, wherein the first and second damping means (34) are located equidistant from the gear. 請求項１から９のいずれか一項に記載の少なくとも１つの減速機（１０）を備えることを特徴とする、ターボ機械。   Turbomachine, characterized in that it comprises at least one speed reducer (10) according to any one of the preceding claims.
JP2018516059A 2014-09-30 2016-09-20 Load distribution of reducer with two intermediate transmission lines Active JP6839704B2 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR1459282A FR3026452B1 (en) 2014-09-30 2014-09-30 SPEED REDUCER WITH TWO INTERMEDIATE TRANSMISSION LINES
FR1559295A FR3026453B1 (en) 2014-09-30 2015-09-30 DISTRIBUTION OF LOADS IN A TRANSMISSION SPEED REDUCER WITH TWO INTERMEDIATE LINES
FR1559295 2015-09-30
PCT/FR2016/052380 WO2017055707A1 (en) 2014-09-30 2016-09-20 Load distribution in a speed reducer with two intermediate transmission lines

Publications (2)

Publication Number Publication Date
JP2018530720A true JP2018530720A (en) 2018-10-18
JP6839704B2 JP6839704B2 (en) 2021-03-10

Family

ID=52102831

Family Applications (2)

Application Number Title Priority Date Filing Date
JP2017516464A Expired - Fee Related JP6677719B2 (en) 2014-09-30 2015-09-18 Reducer with two intermediate transmission lines
JP2018516059A Active JP6839704B2 (en) 2014-09-30 2016-09-20 Load distribution of reducer with two intermediate transmission lines

Family Applications Before (1)

Application Number Title Priority Date Filing Date
JP2017516464A Expired - Fee Related JP6677719B2 (en) 2014-09-30 2015-09-18 Reducer with two intermediate transmission lines

Country Status (8)

Country Link
US (2) US10443697B2 (en)
EP (2) EP3201492B1 (en)
JP (2) JP6677719B2 (en)
CN (2) CN107076029A (en)
CA (2) CA2962328A1 (en)
FR (2) FR3026452B1 (en)
RU (2) RU2688494C2 (en)
WO (2) WO2016051045A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3026452B1 (en) * 2014-09-30 2016-10-28 Hispano Suiza Sa SPEED REDUCER WITH TWO INTERMEDIATE TRANSMISSION LINES
FR3044730B1 (en) * 2015-12-02 2017-12-22 Hispano Suiza Sa TWO LINE TRANSMITTER SPEED REDUCER FOR TURBOPROPULSEUR, TURBOPROPULSEUR COMPRISING SUCH REDUCER
JP6796509B2 (en) * 2017-02-14 2020-12-09 三菱重工業株式会社 Power transmission device
FR3108308B1 (en) 2020-03-19 2024-01-19 Safran Trans Systems DEVICE FOR DRIVING AT LEAST ONE WHEEL OF AN AIRCRAFT LANDING GEAR
FR3128750B1 (en) 2021-11-03 2024-03-15 Safran Trans Systems SPEED REDUCER WITH TWO INTERMEDIATE TRANSMISSION LINES
US11519338B1 (en) * 2022-01-19 2022-12-06 Raytheon Technologies Corporation Gear train with variable input direction of rotation and constant output direction of rotation

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0534342U (en) * 1991-10-11 1993-05-07 石川島播磨重工業株式会社 Gear device
US5542311A (en) * 1993-07-30 1996-08-06 Maag Getriebe Ag Toothed-wheel gear with parallel shafts
JP2006057653A (en) * 2004-08-17 2006-03-02 Kawasaki Heavy Ind Ltd Bearing vibration damping mechanism

Family Cites Families (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH85773A (en) * 1919-05-10 1920-12-01 Bbc Brown Boveri & Cie Gear transmission.
US1503919A (en) * 1921-04-14 1924-08-05 Westinghouse Gear And Dynamome Gearing
FR727162A (en) * 1931-10-30 1932-06-14 Maison Breguet Transformation by gears with two intermediate crews
FR992376A (en) * 1944-06-24 1951-10-17 Cem Comp Electro Mec Elastic mounting device for gear transmission bearings
GB633971A (en) * 1947-09-12 1949-12-30 Frederick Errington Improvements in or relating to spur gearing
US2595513A (en) * 1950-04-28 1952-05-06 Cureton William Coupling for rotating shafts
GB706070A (en) * 1951-02-03 1954-03-24 Fiat Spa Improvements in or relating to gas turbine propelling units for motor vehicles
US2895342A (en) * 1955-07-29 1959-07-21 Thomas S Hayhurst Gearing
US2978885A (en) * 1960-01-18 1961-04-11 Orenda Engines Ltd Rotary output assemblies
FR1583426A (en) * 1968-02-29 1969-10-31
US3772934A (en) * 1971-11-15 1973-11-20 R Warren Floating helical gear
FR2221981A5 (en) * 1973-03-14 1974-10-11 France Etat
US4312244A (en) * 1980-04-24 1982-01-26 United Technologies Corporation Power gearing
DE3018610C2 (en) * 1980-05-13 1982-08-19 Mannesmann AG, 4000 Düsseldorf Multi-way gearboxes with load balancing, especially for ships
WO1985001334A1 (en) * 1983-09-17 1985-03-28 Fujihensokuki Co., Ltd. Gear apparatus
DE3527003A1 (en) * 1985-07-27 1987-05-27 Flender A F & Co Transmission for double-screw machines
DE3543926A1 (en) * 1985-12-12 1987-06-25 Tacke Kg F TRANSMISSION FOR ONE OR MULTIPLE DRIVE
SU1352090A1 (en) * 1985-12-13 1987-11-15 Центральный научно-исследовательский автомобильный и автомоторный институт Gas turbine for power unit reduction gear
DE3712444A1 (en) * 1987-04-11 1988-10-27 Kuehnle Kopp Kausch Ag EXHAUST TURBOCHARGER STORAGE
DE3809577A1 (en) * 1988-03-22 1989-10-12 Messerschmitt Boelkow Blohm MECHANICAL TRANSMISSION
JPH0569982A (en) * 1991-09-12 1993-03-23 Mitsubishi Electric Corp Rotation torque transmission mechanism
US5472386A (en) * 1994-05-26 1995-12-05 United Technologies Corporation Stacked compound planetary gear train for an upgraded powertrain system for a helicopter
JPH1159593A (en) * 1997-08-14 1999-03-02 Fuji Heavy Ind Ltd Power transmission device for helicopter
WO2000017540A2 (en) * 1998-09-18 2000-03-30 Allison Engine Company, Inc. Propeller gearbox
DE29819820U1 (en) * 1998-11-06 1999-01-21 Piv Antrieb Reimers Kg Werner Gearbox especially for twin screw extruders
US6619157B1 (en) * 2001-06-25 2003-09-16 William Bruce Morrow Fluid actuated system for balancing of loads in multi-path geared transmissions
US8015900B2 (en) * 2003-07-16 2011-09-13 Sikorsky Aircraft Corporation Split-torque gear box
US7975465B2 (en) * 2003-10-27 2011-07-12 United Technologies Corporation Hybrid engine accessory power system
JP4539128B2 (en) * 2004-03-09 2010-09-08 オイレス工業株式会社 Rack guide for rack and pinion type steering system
US7624657B2 (en) * 2006-07-12 2009-12-01 Thermotion Corporation Motor-driven actuator
CN101535128B (en) * 2006-11-14 2013-06-12 贝尔直升机泰克斯特龙公司 Multiple drive-path transmission with torque-splitting differential mechanism
CN101201099B (en) * 2007-12-20 2012-06-13 中国科学院长春光学精密机械与物理研究所 Mechanism for unhitching and resetting worm wheel endless screw
US8453539B2 (en) * 2008-06-04 2013-06-04 Crown Iron Works Company Gearbox apparatus and method of manufacture
JP5120110B2 (en) * 2008-06-30 2013-01-16 日本精工株式会社 Electric power steering device
GB2471512A (en) * 2009-07-03 2011-01-05 Smart Mfg Technology Ltd Gear set with helical gears which move axially to reduce imbalanced loads
FR2949834B1 (en) * 2009-09-10 2011-10-07 Conseil Et Tech SHOCK ABSORBER DEVICE
JP5445942B2 (en) * 2009-12-25 2014-03-19 株式会社リコー Drive transmission device, drive device, and image forming apparatus
US8997500B2 (en) * 2010-02-19 2015-04-07 United Technologies Corporation Gas turbine engine oil buffering
WO2011107383A1 (en) * 2010-03-01 2011-09-09 Thyssenkrupp Polysius Ag Drive for a rotary drum
DE102010062047A1 (en) * 2010-11-26 2012-05-31 Zf Friedrichshafen Ag Device for reducing the game in a transmission
FR2989140B1 (en) * 2012-04-06 2014-09-05 Snecma POWER TRANSMISSION SYSTEM FOR A TURBOMACHINE
CN102788143A (en) * 2012-07-30 2012-11-21 邵文远 Automatic gap eliminating servo reducing mechanism
CN103438119A (en) * 2013-09-01 2013-12-11 韩凤琳 Inserter-connected electromagnetic drive clutch with spline shafts having discs and spline sleeves having discs
FR3026452B1 (en) * 2014-09-30 2016-10-28 Hispano Suiza Sa SPEED REDUCER WITH TWO INTERMEDIATE TRANSMISSION LINES

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0534342U (en) * 1991-10-11 1993-05-07 石川島播磨重工業株式会社 Gear device
US5542311A (en) * 1993-07-30 1996-08-06 Maag Getriebe Ag Toothed-wheel gear with parallel shafts
JP2006057653A (en) * 2004-08-17 2006-03-02 Kawasaki Heavy Ind Ltd Bearing vibration damping mechanism

Also Published As

Publication number Publication date
EP3201492A1 (en) 2017-08-09
WO2016051045A1 (en) 2016-04-07
CA3000090A1 (en) 2017-04-06
EP3356699B1 (en) 2020-05-27
CN108027019A (en) 2018-05-11
JP2017532509A (en) 2017-11-02
JP6677719B2 (en) 2020-04-08
RU2017109880A3 (en) 2019-04-11
FR3026453A1 (en) 2016-04-01
RU2688494C2 (en) 2019-05-21
CN108027019B (en) 2021-11-12
EP3201492B1 (en) 2022-11-16
FR3026452B1 (en) 2016-10-28
US20180372197A1 (en) 2018-12-27
CN107076029A (en) 2017-08-18
WO2017055707A1 (en) 2017-04-06
JP6839704B2 (en) 2021-03-10
RU2720022C1 (en) 2020-04-23
FR3026452A1 (en) 2016-04-01
RU2017109880A (en) 2018-11-05
US10443697B2 (en) 2019-10-15
EP3356699A1 (en) 2018-08-08
FR3026453B1 (en) 2016-11-04
US20170321787A1 (en) 2017-11-09
CA2962328A1 (en) 2016-04-07

Similar Documents

Publication Publication Date Title
JP6839704B2 (en) Load distribution of reducer with two intermediate transmission lines
JP6490676B2 (en) Planetary carrier for epicyclic reduction gears
CN103987941B (en) Fan drive gear system for gas turbine engine and gas turbine engine
US8672801B2 (en) Mounting system for a planetary gear train in a gas turbine engine
CN109923335B (en) Planet carrier for reduction unit with planetary gear train
CN104220729A (en) Gearbox and turbine engine with geared fan
US20130089284A1 (en) Method for dynamically absorbing shocks in a power shaft, in particular a supercritical shaft, and shock-absorbing architecture for implementing said method
US10119548B2 (en) Aircraft engine with a compressor device
US20180230902A1 (en) Planetary gearbox for gas turbine engine
CN108317238B (en) Planetary gear system arrangement with auxiliary oil system
CN105899794A (en) Epicyclic reduction device for the rotational drive of blade sets of a reduction turbomachine
GB2544869A (en) Turbojet engine with offset fans with a diffrential system
CN108138658A (en) The turbogenerator of deceleration device with fan and in power turbine shaft
GB2548140A (en) Transmission system
JP2018515723A (en) Reducer with two intermediate transmission lines
JP6636029B2 (en) Manufacturing method of propeller speed reducer
US20180149235A1 (en) Power transmission mechanism
JP6799598B2 (en) A speed reducer having two intermediate lines for a turboprop engine, a turboprop engine including the speed reducer
KR102133065B1 (en) Transmission arrangement for a ship's drive and ship's drive with a transmission arrangement
RU2655968C1 (en) Power plant planetary gearbox
CN108626378A (en) Planet stent and epicyclic gearing for epicyclic gearing
WO2011072601A1 (en) Geared drive system with load sharing
CN109282017A (en) Gear assembly for aerospace applications
EP3663542A3 (en) Oil supply arrangement for bearing
CN110259913A (en) Duct-Burning Turbofan, star gear train case and herringbone gear installation

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20190905

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20200813

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20200825

A601 Written request for extension of time

Free format text: JAPANESE INTERMEDIATE CODE: A601

Effective date: 20201120

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20210115

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20210209

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20210215

R150 Certificate of patent or registration of utility model

Ref document number: 6839704

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150